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LEMUR-2-MYRA, 66787

Orbit data source: Space-Track

LEMUR-2-MYRA, 66787 is an American payload satellite in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
66787, 2025-276EC
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
2025-11-28 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 LEMUR-2-MYRA
1 66787U 25276EC  26141.17768219  .00003273  00000-0  26826-3 0  9993
2 66787  97.5249 212.9495 0013268 231.9415 128.0613 14.99875588 26169
Epoch: 2026-05-21T04:15Z
TLE epoch observation values (Epoch: 2026-05-21T04:15:51.741Z)
Latitude
0.00005°
Longitude
-89.84272°
Altitude
576.03 km
Speed
7.57 km/s
True Right ascension
14h 11m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:08:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.489 km
Perigee altitude
555.067 km
Semi-major axis
6,942.415 km
Eccentricity
0.00133
Inclination
97.5249°
RAAN
212.9495°
Arg. of periapsis
231.9415°
True anomaly
128.18089°
Mean anomaly
128.0613°
Eccentric anomaly
128.12111°
Mean motion
3.75212 °/min
Orbital period
95.95 mins
BSTAR
0.00026826
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Documentation

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